Project Details
Description
FAA Development of Reliable Modeling Methodologies for Fan Blade Out Containment Analysis FAA Development of Reliable Modeling Methodologies for Fan Blade Out Containment Analysis High-Strain Rate Testing of Fabrics Used in Engine Containment Systems
| Status | Finished |
|---|---|
| Effective start/end date | 10/1/03 → 9/11/07 |
Funding
- DOT: Federal Aviation Administration (FAA): $832,889.00
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